US20240136895A1 - Method of repairing a hydrogenerator - Google Patents
Method of repairing a hydrogenerator Download PDFInfo
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- US20240136895A1 US20240136895A1 US18/537,203 US202318537203A US2024136895A1 US 20240136895 A1 US20240136895 A1 US 20240136895A1 US 202318537203 A US202318537203 A US 202318537203A US 2024136895 A1 US2024136895 A1 US 2024136895A1
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K15/00—Processes or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines
- H02K15/50—Disassembling, repairing or modifying dynamo-electric machines
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- H02K15/0006—
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K1/00—Details of the magnetic circuit
- H02K1/06—Details of the magnetic circuit characterised by the shape, form or construction
- H02K1/22—Rotating parts of the magnetic circuit
- H02K1/27—Rotor cores with permanent magnets
- H02K1/2706—Inner rotors
- H02K1/272—Inner rotors the magnetisation axis of the magnets being perpendicular to the rotor axis
- H02K1/274—Inner rotors the magnetisation axis of the magnets being perpendicular to the rotor axis the rotor consisting of two or more circumferentially positioned magnets
- H02K1/2753—Inner rotors the magnetisation axis of the magnets being perpendicular to the rotor axis the rotor consisting of two or more circumferentially positioned magnets the rotor consisting of magnets or groups of magnets arranged with alternating polarity
- H02K1/278—Surface mounted magnets; Inset magnets
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B13/00—Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates
- F03B13/08—Machine or engine aggregates in dams or the like; Conduits therefor, e.g. diffusors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B13/00—Adaptations of machines or engines for special use; Combinations of machines or engines with driving or driven apparatus; Power stations or aggregates
- F03B13/08—Machine or engine aggregates in dams or the like; Conduits therefor, e.g. diffusors
- F03B13/083—The generator rotor being mounted as turbine rotor rim
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C43/00—Assembling bearings
- F16C43/02—Assembling sliding-contact bearings
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
- G01N29/04—Analysing solids
- G01N29/043—Analysing solids in the interior, e.g. by shear waves
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
- G01N29/34—Generating the ultrasonic, sonic or infrasonic waves, e.g. electronic circuits specially adapted therefor
- G01N29/348—Generating the ultrasonic, sonic or infrasonic waves, e.g. electronic circuits specially adapted therefor with frequency characteristics, e.g. single frequency signals, chirp signals
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K1/00—Details of the magnetic circuit
- H02K1/06—Details of the magnetic circuit characterised by the shape, form or construction
- H02K1/22—Rotating parts of the magnetic circuit
- H02K1/28—Means for mounting or fastening rotating magnetic parts on to, or to, the rotor structures
- H02K1/30—Means for mounting or fastening rotating magnetic parts on to, or to, the rotor structures using intermediate parts, e.g. spiders
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/18—Structural association of electric generators with mechanical driving motors, e.g. with turbines
- H02K7/1807—Rotary generators
- H02K7/1823—Rotary generators structurally associated with turbines or similar engines
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2230/00—Manufacture
- F05B2230/80—Repairing, retrofitting or upgrading methods
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/04—Sliding-contact bearings for exclusively rotary movement for axial load only
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2360/00—Engines or pumps
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2291/00—Indexing codes associated with group G01N29/00
- G01N2291/02—Indexing codes associated with the analysed material
- G01N2291/028—Material parameters
- G01N2291/0289—Internal structure, e.g. defects, grain size, texture
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2291/00—Indexing codes associated with group G01N29/00
- G01N2291/04—Wave modes and trajectories
- G01N2291/044—Internal reflections (echoes), e.g. on walls or defects
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2291/00—Indexing codes associated with group G01N29/00
- G01N2291/26—Scanned objects
- G01N2291/269—Various geometry objects
- G01N2291/2693—Rotor or turbine parts
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K2213/00—Specific aspects, not otherwise provided for and not covered by codes H02K2201/00 - H02K2211/00
- H02K2213/06—Machines characterised by the presence of fail safe, back up, redundant or other similar emergency arrangements
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B10/00—Integration of renewable energy sources in buildings
- Y02B10/50—Hydropower in dwellings
Definitions
- the present disclosure relates to a method of repairing a hydrogenerator.
- Hydroelectric power comes from flowing water, for example, winter and spring runoff from mountain streams and clear lakes. Water, when it is falling by the force of gravity, can be used to turn turbines and generators that produce electricity.
- hydropower is generated.
- Some powerplants are located on rivers, streams, and canals, but for a reliable water supply, dams are needed. Dams store water for later release for such purposes as irrigation, domestic and industrial use, and power generation.
- the reservoir acts much like a battery, storing water to be released as needed to generate power.
- FIG. 1 illustrates a hydropower plant that includes an upper body of water 10 feeding a turbine 1 through a pressure line 20 via a shutoff element 30 .
- the turbine 1 drives a generator 40 that generates electricity.
- the turbine 1 and the electric generator 40 together form a hydrogenerator (hydroelectric generator) 70 .
- a dam creates a reservoir forming the upper body of water 10 .
- the reservoir has a “head” or height from which water flows.
- a pipe penstock carries the water from the reservoir to the hydrogenerator 70 .
- the hydrogenerator 70 shown in FIG. 2 is a vertical hydrogenerator designed around a vertically mounted shaft assembly. Attached to the upper portion of the shaft assembly is a rotor 100 (see FIG. 3 A ) of the generator 40 . Attached to the lower end of the shaft is the turbine 1 .
- the turbine 1 has turbine blades driven by the fast-moving water from the penstock, something like a pinwheel in the wind.
- the turbine 1 drives the rotor 100 within a stator of the electric generator 70 to generate electricity.
- FIG. 3 A shows a rotor 100 of a typical electric generator 40
- FIG. 3 B shows a cross-section of the circled portion of the rotor 100 in FIG. 3 A
- the rotor 100 includes a shaft 102 and a spider 103 attached to the shaft 102 .
- the spider 103 supports a rim 108 surrounding the shaft 102 .
- the rim 108 carries a number of poles 110 spaced along the outer circumference of the rim 108 .
- the electric generator 70 generates electricity.
- the illustrated spider 103 is a welded steel structure having six spider arms 104 with vertical posts 105 at their ends that support the rim 108 .
- the rim 108 is a ring of laminated steel segments held together by solid steel end plates 109 at the top and bottom, and clamped together by bolts 130 (see FIG. 6 ) passing through the end plates and laminations.
- the rotor poles 110 in turn are supported by the rim 108 both radially, usually by dovetails, and axially by the rim 108 .
- the weight of the rotor 100 and the rim 108 are supported on the vertical posts 105 of the spider arms 104 .
- Each vertical post 105 is provided with a rim support ledge 106 machined in the base of the vertical post.
- FIG. 3 C shows a close-up view of a rim support ledge 106 machined in the base of the vertical post 105 .
- the rim 108 is supported on the rim support ledges 106 , and is mounted on the spider arms 104 by a friction fit.
- a common problem that occurs in the operation of the electric generator 40 is that wear occurs at the rim support ledge 106 generally due to friction between the rim 108 and the rim support ledge 106 . Because of different operational forces and other factors, the rim 108 may move with respect to the rim support ledge 106 , which can ultimately lead to damage, such as the fracture 112 of the rim support ledge 106 illustrated in FIG. 3 C .
- Examples of operational forces that may cause the rim 108 to move with respect to one or more of the rim support ledges 106 include high frequency forces that may occur once or twice with each revolution of the rotor 100 : eccentricity (out of roundness) of the rotor 100 ; and unbalanced magnetic forces that can distort the rim 108 .
- FIG. 4 An unbalanced magnetic pole vector V on the rotor 100 is shown in FIG. 4 .
- the clearance 114 at the top of FIG. 4 is shown as the clearance with the rim 108 concentric.
- the eccentricity 116 at the bottom of FIG. 4 is shown as clearance with the rim 108 eccentric.
- the magnetic forces distort the rim 108 during operation whereby, because of the rim's construction in layers, fretting or other wear occurs which ultimately leads to the failure of some part of the rotor structure which then must be repaired.
- the lateral flexibility of the spider arms 104 plus the loss of frictional interference between the rim 108 and the spider arms 104 permits the rim 108 to slide on the ledges 106 at each start, and also once per revolution, when exposed to an unbalanced magnetic pole.
- Examples of operational forces that may cause the rim 108 to move with respect to one or more of the rim support ledges 106 include low cycle forces that occur with start/stop of the hydrogenerator 70 or arise from transient operating conditions: radial expansion of the rim 108 caused by rotation of the rim 108 ; differential radial expansion of the rim 108 caused by the rim 108 heating more than the spider 103 during operation; stopping and cooling of the rim 108 when the hydrogenerator 70 is shut down; and overspeed/runaway conditions, out-of-phase synchronizations, short circuits, and transient torque spikes.
- FIG. 5 A shows the force 118 of the dead weight of the rim 108 and the poles 110 pulling down on the spider arms 104 .
- FIG. 5 B shows the traction (friction) force 120 from sliding, which forces combine to cause wear during operation.
- the dead weight of the rim 108 and the poles 110 will act upon components of the hydroelectric generator 70 .
- At each start and stop of the hydroelectric generator 70 there will be a centrifugal force on the generator rim 108 , thereby causing the components thereof to move with respect to one another.
- the movement of the components with respect to one another will cause or contribute in causing the fretting or other damage to the components of the rotor 100 , which will accelerate damage and the appearance of cracks in the structure of the rotor 100 .
- rim support ledges are where fatigue and wear caused by the relative movement of the rim can occur. The wear can produce cracking and eventually even a complete fracture or breaking off of a rim support ledge. Since the ledges provide support for the rim, breakage of these ledges could result in significant damage to the rotor as a whole and individual components thereof, as well as any adjacent portions of the hydrogenerator.
- the repair method involves the rim being supported from the top of the spider posts instead of on the rim support ledges at the bottom of the spider posts.
- support structures are attached to the tops of the spider posts to support the rim from above and relieve the weight on the rim support ledges.
- Embodiments of the support structures are thrust plates formed from steel having sufficient strength to support the rim while preserving ductility and toughness for fatigue resistance.
- the thrust plates can be affixed to the rim with sleeve bolts that thread to the rim clamping studs.
- the sleeve bolts can be tightened periodically to compensate for wear of the thrust plates or to compensate for wear of wear plates placed below the thrust plates.
- the disclosed method for repair hangs the rim from the top of the spider posts.
- the disclosed method has a number of advantages:
- FIG. 1 shows a possible hydropower plant
- FIG. 2 is a diagram of how a hydropower plant works
- FIGS. 3 A, 3 B, and 3 C show a typical geometry and failure location of a rotor
- FIG. 4 shows an unbalanced magnetic pole vector on a rotor
- FIG. 5 A shows the dead weight of the rim and the poles of a rotor
- FIG. 5 B shows the traction (friction) force from sliding.
- FIGS. 6 and 7 show an embodiment of a thrust plate assembly for a hydrogenerator in place on the rotor shown in FIG. 3 ;
- FIG. 8 is a top view of the thrust plate of the thrust plate assembly shown in FIG. 7 .
- FIG. 6 shows a thrust plate assembly having a thrust plate 122 used in an embodiment of the disclosed method for repairing the electric generator 40 shown in FIGS. 3 A and 3 C as having a fractured rim support ledge 106 .
- a plurality of thrust plates 122 are located one at each of a corresponding spider arm 104 .
- the thrust plates 122 support the rim 108 from above on the spider arms 104 .
- the weight of the rim 108 is supported by the thrust plates 122 , such that the rim 108 is, in a sense, hanging from the thrust plates 122 .
- the thrust plate 122 is spaced apart from the rim 108 itself.
- a wear plate or sacrificial plate 124 is located in a recessed or stepped or shoulder portion 126 of the thrust plate 122 between the thrust plate 122 and the spider arm 104 .
- a portion of the wear plate 124 may or may not extend so as to be in contact with the top of the rim 108 .
- the spacing of the thrust plate 122 a distance from the rim 108 prevents frictional contact between the thrust plate 122 and the rim 108 , and thus prevents wear.
- the wear plate 124 which is lubricated with a solid lubricant, experiences friction and wear.
- a sleeve bolt 128 can be tightened periodically to tighten the connection of the thrust plate 122 . In this manner, the life of the rotor 100 can be extended without extensive repairs or replacement.
- FIG. 7 illustrates mounting of a thrust plate 122 on the rim 108 adjacent to a spider arm vertical post 105
- FIG. 8 illustrates the fasteners fastening the thrust plate 122 on the rim top plate 109
- the thrust plates 122 can be 3′′ (three inch) thick machined plates manufactured from ASTM A829 SAE 4140 with a minimum yield strength of 70 ksi, and a UTS not less than 118 ksi and a40% reduction in area. This provides strength while providing ductility and toughness for fatigue resistance.
- Each thrust plate 122 is affixed to the rim 108 with five sleeve bolts 128 that thread to the rim clamping studs 130 (see FIG. 6 ), and two 1.25′′ (one-and-one-quarter inch) alloy socket head cap screws 132 .
- the sleeve bolts 128 are modeled for stress analysis as though a 2.75′′ (two- and three-quarters inch) Hex bolt with a suitable length of unthreaded shank were cut off, bored and tapped with 1.75′′-5 UNC inside threads. The minimum tensile area of this configuration is slightly greater than that of the original stud.
- the sleeve bolts 128 are made from commercial Grade 5 bolts, and thus will be at least as strong as the rim studs 130 . The length below the heads will be 3′′ (three inches); then with the washers under the head, contact of the bottom of the shank with the rim top plate 109 will be avoided.
- the two 1.25′′ (one-and-one-quarter inch) socket head cap screws 132 are used to resist localized bending due to the weight of the rim 108 .
- the design specification calls for a maximum of 1 ⁇ 3rd (one-third) of the rim weight to be carried by an individual thrust plate 122 . This is slightly over 33 tons for the illustrated rim, and though obviously could not be carried by all of the thrust plates 122 , could conceivably be carried by some of them.
- the rim top plate 109 must be drilled and tapped for the Helicoil thread insert corresponding to this thread.
- the rim could be lifted from the support ledges. This makes it possible to control the loading scenario so that the spider arms will carry only 1 ⁇ 6th (not 1 ⁇ 3rd) of the rim load each, as a steady load. With careful friction control, then, the stress ranges due to rim movement on the bearing surfaces may be lowered. As well, there will be no unloading of the rim weight as is posited in the low cycle fatigue scenario.
- the spider is designed with uneven angular spacing of the rotor spider arms.
- the intent was to make the rim as close to “elastically solid” as possible. That is to say that slipping between laminations, which would allow the rim to grow circumferentially leading to a loss of interference with the spider, is prevented (or attempted to be prevented) by high friction forces and close fitting of the clamping bolts to the holes in the laminations.
- Rim ledge cracking is ordinarily a high cycle fatigue problem caused by the normal imperfections of operation in combination with rim dead weight loading and the frictional forces on the rim ledge due to rim movement.
- These “normal imperfections” include such things as eccentricity of the rotor in the stator, unbalanced magnetic pull, and the elastic deformation of the rotor and stator. This causes the push-pull frictional forces noted above to increase in frequency from once or (a few times) per start-stop cycle to once or twice per revolution, a clearly different fatigue regime in which millions of cycles occur relatively quickly. As an example, suppose these machines were started and stopped once per day; then 365 cycles/year would occur. But if they were operated even 12 hours/day at 277 rpm, 457 million cycles would occur in 1 year.
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Abstract
Description
- This application is a continuation of U.S. patent application Ser. No. 16/974,278, filed Dec. 14, 2020, which is incorporated herein by reference in its entirety.
- The present disclosure relates to a method of repairing a hydrogenerator.
- Background information is for informational purposes only and does not necessarily admit that subsequently mentioned information and publications are prior art.
- Hydroelectric power comes from flowing water, for example, winter and spring runoff from mountain streams and clear lakes. Water, when it is falling by the force of gravity, can be used to turn turbines and generators that produce electricity.
- At facilities called hydroelectric powerplants, hydropower is generated. Some powerplants are located on rivers, streams, and canals, but for a reliable water supply, dams are needed. Dams store water for later release for such purposes as irrigation, domestic and industrial use, and power generation. The reservoir acts much like a battery, storing water to be released as needed to generate power.
-
FIG. 1 illustrates a hydropower plant that includes an upper body ofwater 10 feeding aturbine 1 through apressure line 20 via ashutoff element 30. Theturbine 1 drives agenerator 40 that generates electricity. Theturbine 1 and theelectric generator 40 together form a hydrogenerator (hydroelectric generator) 70. - As shown in
FIG. 2 , a dam creates a reservoir forming the upper body ofwater 10. The reservoir has a “head” or height from which water flows. A pipe (penstock) carries the water from the reservoir to thehydrogenerator 70. Thehydrogenerator 70 shown inFIG. 2 is a vertical hydrogenerator designed around a vertically mounted shaft assembly. Attached to the upper portion of the shaft assembly is a rotor 100 (seeFIG. 3A ) of thegenerator 40. Attached to the lower end of the shaft is theturbine 1. Theturbine 1 has turbine blades driven by the fast-moving water from the penstock, something like a pinwheel in the wind. Theturbine 1 drives therotor 100 within a stator of theelectric generator 70 to generate electricity. -
FIG. 3A shows arotor 100 of a typicalelectric generator 40, andFIG. 3B shows a cross-section of the circled portion of therotor 100 inFIG. 3A . Therotor 100 includes ashaft 102 and aspider 103 attached to theshaft 102. Thespider 103 supports arim 108 surrounding theshaft 102. Therim 108 carries a number ofpoles 110 spaced along the outer circumference of therim 108. When thepoles 110 pass by poles in the stator during rotation of therotor 100, theelectric generator 70 generates electricity. - The illustrated
spider 103 is a welded steel structure having sixspider arms 104 withvertical posts 105 at their ends that support therim 108. Therim 108 is a ring of laminated steel segments held together by solidsteel end plates 109 at the top and bottom, and clamped together by bolts 130 (seeFIG. 6 ) passing through the end plates and laminations. Therotor poles 110 in turn are supported by therim 108 both radially, usually by dovetails, and axially by therim 108. - The weight of the
rotor 100 and therim 108 are supported on thevertical posts 105 of thespider arms 104. Eachvertical post 105 is provided with a rim support ledge 106 machined in the base of the vertical post.FIG. 3C shows a close-up view of a rim support ledge 106 machined in the base of thevertical post 105. In general, therim 108 is supported on the rim support ledges 106, and is mounted on thespider arms 104 by a friction fit. - A common problem that occurs in the operation of the
electric generator 40 is that wear occurs at therim support ledge 106 generally due to friction between therim 108 and therim support ledge 106. Because of different operational forces and other factors, therim 108 may move with respect to therim support ledge 106, which can ultimately lead to damage, such as thefracture 112 of therim support ledge 106 illustrated inFIG. 3C . - Examples of operational forces that may cause the
rim 108 to move with respect to one or more of the rim support ledges 106 include high frequency forces that may occur once or twice with each revolution of the rotor 100: eccentricity (out of roundness) of therotor 100; and unbalanced magnetic forces that can distort therim 108. - An unbalanced magnetic pole vector V on the
rotor 100 is shown inFIG. 4 . Theclearance 114 at the top ofFIG. 4 is shown as the clearance with therim 108 concentric. Theeccentricity 116 at the bottom ofFIG. 4 is shown as clearance with therim 108 eccentric. The magnetic forces distort therim 108 during operation whereby, because of the rim's construction in layers, fretting or other wear occurs which ultimately leads to the failure of some part of the rotor structure which then must be repaired. The lateral flexibility of thespider arms 104 plus the loss of frictional interference between therim 108 and thespider arms 104 permits therim 108 to slide on theledges 106 at each start, and also once per revolution, when exposed to an unbalanced magnetic pole. It is very difficult if not impossible to build a hydrogenerator which does not have an unbalance magnetic pole. Even the slightest unbalance will cause the components of the rotor to move with respect to one another and cause fretting if not other wear on the rotor. - Examples of operational forces that may cause the
rim 108 to move with respect to one or more of the rim support ledges 106 include low cycle forces that occur with start/stop of thehydrogenerator 70 or arise from transient operating conditions: radial expansion of therim 108 caused by rotation of therim 108; differential radial expansion of therim 108 caused by therim 108 heating more than thespider 103 during operation; stopping and cooling of therim 108 when thehydrogenerator 70 is shut down; and overspeed/runaway conditions, out-of-phase synchronizations, short circuits, and transient torque spikes. -
FIG. 5A shows theforce 118 of the dead weight of therim 108 and thepoles 110 pulling down on thespider arms 104.FIG. 5B shows the traction (friction) force 120 from sliding, which forces combine to cause wear during operation. The dead weight of therim 108 and thepoles 110 will act upon components of thehydroelectric generator 70. At each start and stop of thehydroelectric generator 70 there will be a centrifugal force on thegenerator rim 108, thereby causing the components thereof to move with respect to one another. The movement of the components with respect to one another will cause or contribute in causing the fretting or other damage to the components of therotor 100, which will accelerate damage and the appearance of cracks in the structure of therotor 100. - In general, hydrogenerators often experience fatigue cracking of the rotor rim support ledges. The rim support ledges are where fatigue and wear caused by the relative movement of the rim can occur. The wear can produce cracking and eventually even a complete fracture or breaking off of a rim support ledge. Since the ledges provide support for the rim, breakage of these ledges could result in significant damage to the rotor as a whole and individual components thereof, as well as any adjacent portions of the hydrogenerator.
- The most common approaches to repair damaged rim support ledges are to either remove and then replace or refurbish the rim, or to provide supplemental supports beneath the rim or in the rim vent duct. Replacement or refurbishment is undesirable as it is very expensive, time-consuming, and requires complete removal or lifting of the rim. Supplemental supports beneath the rim are not usually able to carry the full load of the rim and have poor resistance to fatigue. Supplemental supports in the rim vent duct have the problems of not being applicable to all machines, difficulty in achieving load sharing, and having an indeterminate lifespan.
- Thus, there is a need to provide a cost-effective repair method for hydrogenerators to extend the life span of a rim and spider of a rotor upon damage to the rim support ledges.
- Disclosed is a cost-effective repair method for hydrogenerators that extends the life span of a rim and spider of a rotor upon damage to the rim support ledges.
- According to one possible embodiment, the repair method involves the rim being supported from the top of the spider posts instead of on the rim support ledges at the bottom of the spider posts. In general, support structures are attached to the tops of the spider posts to support the rim from above and relieve the weight on the rim support ledges.
- Embodiments of the support structures are thrust plates formed from steel having sufficient strength to support the rim while preserving ductility and toughness for fatigue resistance. The thrust plates can be affixed to the rim with sleeve bolts that thread to the rim clamping studs. The sleeve bolts can be tightened periodically to compensate for wear of the thrust plates or to compensate for wear of wear plates placed below the thrust plates.
- The disclosed method for repair hangs the rim from the top of the spider posts. The disclosed method has a number of advantages:
-
- 1. It replaces the rim ledge with a considerably stronger piece of material that is still ductile and has excellent fatigue resistance;
- 2. The support structures have a greatly reduced stress concentration at the corner of the support as compared to the rim ledges;
- 3. The support structures control the friction between the rim support and the spider post; and
- 4. The support structures reset the “fatigue cycles” counter to zero with respect to support of the rim on the spider.
-
FIG. 1 shows a possible hydropower plant; -
FIG. 2 is a diagram of how a hydropower plant works; -
FIGS. 3A, 3B, and 3C show a typical geometry and failure location of a rotor; -
FIG. 4 shows an unbalanced magnetic pole vector on a rotor; -
FIG. 5A shows the dead weight of the rim and the poles of a rotor, andFIG. 5B shows the traction (friction) force from sliding. -
FIGS. 6 and 7 show an embodiment of a thrust plate assembly for a hydrogenerator in place on the rotor shown inFIG. 3 ; and -
FIG. 8 is a top view of the thrust plate of the thrust plate assembly shown inFIG. 7 . -
FIG. 6 shows a thrust plate assembly having athrust plate 122 used in an embodiment of the disclosed method for repairing theelectric generator 40 shown inFIGS. 3A and 3C as having a fracturedrim support ledge 106. - In general, in this embodiment a plurality of
thrust plates 122 are located one at each of acorresponding spider arm 104. Thethrust plates 122 support therim 108 from above on thespider arms 104. In other words, instead of the weight of therim 108 resting solely on therim support ledges 106, which one or morerim support ledges 106 are cracked or completely broken off, the weight of therim 108 is supported by thethrust plates 122, such that therim 108 is, in a sense, hanging from thethrust plates 122. Thethrust plate 122 is spaced apart from therim 108 itself. - In the illustrated embodiment a wear plate or
sacrificial plate 124 is located in a recessed or stepped orshoulder portion 126 of thethrust plate 122 between thethrust plate 122 and thespider arm 104. A portion of thewear plate 124 may or may not extend so as to be in contact with the top of therim 108. The spacing of the thrust plate 122 a distance from therim 108 prevents frictional contact between thethrust plate 122 and therim 108, and thus prevents wear. Instead, thewear plate 124, which is lubricated with a solid lubricant, experiences friction and wear. - As the
wear plate 124 wears down, asleeve bolt 128 can be tightened periodically to tighten the connection of thethrust plate 122. In this manner, the life of therotor 100 can be extended without extensive repairs or replacement. - The following discusses the installation, design, and function of the
thrust plate 122 in greater detail. It should be noted that all numbers and materials specifically listed for different parts and components and measurements thereof are strictly in accordance with at least one possible embodiment and should not be understood as limiting the embodiments disclosed herein, as well as any reasonable variations or modifications thereof. -
FIG. 7 illustrates mounting of athrust plate 122 on therim 108 adjacent to a spider armvertical post 105, andFIG. 8 illustrates the fasteners fastening thethrust plate 122 on the rimtop plate 109. Thethrust plates 122 can be 3″ (three inch) thick machined plates manufactured from ASTM A829 SAE 4140 with a minimum yield strength of 70 ksi, and a UTS not less than 118 ksi and a40% reduction in area. This provides strength while providing ductility and toughness for fatigue resistance. Eachthrust plate 122 is affixed to therim 108 with fivesleeve bolts 128 that thread to the rim clamping studs 130 (seeFIG. 6 ), and two 1.25″ (one-and-one-quarter inch) alloy socket head cap screws 132. - The
sleeve bolts 128 are modeled for stress analysis as though a 2.75″ (two- and three-quarters inch) Hex bolt with a suitable length of unthreaded shank were cut off, bored and tapped with 1.75″-5 UNC inside threads. The minimum tensile area of this configuration is slightly greater than that of the original stud. Thesleeve bolts 128 are made from commercial Grade 5 bolts, and thus will be at least as strong as therim studs 130. The length below the heads will be 3″ (three inches); then with the washers under the head, contact of the bottom of the shank with the rimtop plate 109 will be avoided. - The two 1.25″ (one-and-one-quarter inch) socket
head cap screws 132 are used to resist localized bending due to the weight of therim 108. The design specification calls for a maximum of ⅓rd (one-third) of the rim weight to be carried by anindividual thrust plate 122. This is slightly over 33 tons for the illustrated rim, and though obviously could not be carried by all of thethrust plates 122, could conceivably be carried by some of them. The rimtop plate 109 must be drilled and tapped for the Helicoil thread insert corresponding to this thread. - Stress analysis (including the use of finite element models) and both high-cycle fatigue analysis and low cycle fatigue analysis of the thrust plate, rim top plate in the vicinity of its attachment to the thrust plate, and the loading of the fasteners attaching the transfer plate to the top of the rim were conducted. Stresses in the thrust plate, rim top plate in the vicinity of the attachment, and the loading of the socket head cap screws were evaluated. Because the
rim 108 now hangs from the rim'stop end plate 109, stresses in the top end plate are impacted. Also impacted are rim compression and rim studs, which in addition to the clamping load now carry the weight of the rim in an area localized to the thrust plate installation. - Evaluation of the thrust plate, rim, rim top plate and attachment methods under very conservative loading assumptions show that the repair method applied to the
rotor 100 will be suitable for at least a 5 year life, and very likely for a considerable period beyond this if necessary. The conditions necessarily used for evaluation were found to be conservative just as this report was being finalized. That is, it was found that the rotor rims were loose enough to be lifted off the spider arm support ledges. This more certainly fixes the spider post dead weight loading at 1 x the rim weight as a steady load (up-thrusting is eliminated). It was therefore concluded that the thrust plate repair will be suitable for the service intended. - Further, in evaluating the application of the disclosed method for repair to a specific hydrogenerator, it may not be known if it is possible to lift the rim relative to the spider. This can result in a somewhat indeterminate loading situation. The rim would be leveled and the thrust plates would be assembled to a cold rim. At that point the transfer plates would be carrying little load. But as it is unclear how much load cracked ledges might bear (and clearly broken ledges would bear none), a complex load situation may be created. The loading scenario may be based on solid rim support ledges. In order to bound the possibilities of a lack of support from some of the ledges, the possible load on an arm may be increased (for example, doubled).
- It may be that the rim could be lifted from the support ledges. This makes it possible to control the loading scenario so that the spider arms will carry only ⅙th (not ⅓rd) of the rim load each, as a steady load. With careful friction control, then, the stress ranges due to rim movement on the bearing surfaces may be lowered. As well, there will be no unloading of the rim weight as is posited in the low cycle fatigue scenario.
- For some rotors, the spider is designed with uneven angular spacing of the rotor spider arms. Taken together. it appears that the intent was to make the rim as close to “elastically solid” as possible. That is to say that slipping between laminations, which would allow the rim to grow circumferentially leading to a loss of interference with the spider, is prevented (or attempted to be prevented) by high friction forces and close fitting of the clamping bolts to the holes in the laminations.
- In evaluating application of the disclosed method for repair to a specific hydrogenerator, it may not be known if the hydrogenerator rim was designed to “float” duration operation. Hydro generators of similar construction have been designed with floating rims; however, rims utilizing an interference fit relative to the spider are more common. Regardless of the original design, it is accepted that the rim is now floating and likely has been for some time. That is, the rim outgrows the spider due to centrifugal forces and differential heating. This is a small amount of movement and ideally occurs only once per start/stop cycle. This movement creates an alternating “push-pull” on the rim support ledges that is imposed on the steady state stresses due to the dead weight of the rim and poles. Thus, a low cycle fatigue situation would likely exist even under ideal conditions just based on the design and construction, and the rim ledges should have been designed to withstand that scenario. Rim ledge cracking is ordinarily a high cycle fatigue problem caused by the normal imperfections of operation in combination with rim dead weight loading and the frictional forces on the rim ledge due to rim movement. These “normal imperfections” include such things as eccentricity of the rotor in the stator, unbalanced magnetic pull, and the elastic deformation of the rotor and stator. This causes the push-pull frictional forces noted above to increase in frequency from once or (a few times) per start-stop cycle to once or twice per revolution, a clearly different fatigue regime in which millions of cycles occur relatively quickly. As an example, suppose these machines were started and stopped once per day; then 365 cycles/year would occur. But if they were operated even 12 hours/day at 277 rpm, 457 million cycles would occur in 1 year.
- It is impossible to avoid these forces to some degree in any hydro generator. Some manufacturers attempt to prevent the cracking by shrinking the rim onto the spider, so that the rim does not slide on the rim ledge. On these machines, without a specific preload target, it can only be stated that the combination of measures did not prevent the movement. It is also noted that, as these are frictional forces due to sliding, the forces on the rim ledge due to startup and shutdown are of the same magnitude as high cycle forces that cause smaller movements.
- The following patents, patent applications, patent publications, and other documents, except of the exceptions indicated herein, are hereby incorporated by reference as if set forth in their entirety herein except for the exceptions indicated herein, as follows: “The Use of Silver in Self-Lubricating Coatings for Extreme Temperatures” by Harold E. Sliney, prepared for the Annual Meeting of the American Society of Lubrication Engineers, Las Vegas, Nev., May 6-9, 1985; U.S. Pat. No. 8,333,006, having the title “Method for removing a crack in an electromechanical rotor”, issued on Dec. 18, 2012; U.S. Pat. No. 7,866,020, having the title “Method for repairing a crack in an electromechanical rotor, method for preventing crack growth in the same, electromechanical rotor and rotary electrical machine”, issued on Jan. 11, 2011; U.S. Pat. No. 4,636,675, having the title “Rotor spider for rotary electric machine”, issued on Jan. 13, 1987; U.S. Pat. No. 4,327,303, having the title “Rotor assembly for a dynamoelectric machine”, issued on Apr. 27, 1982; U.S. Pat. No. 4,283,648, having the title “Synchronous electric machine with salient poles in the rotor”, issued on Aug. 11, 1981; U.S. Pat. No. 4,182,966, having the title “Ventilation system for dynamoelectric machines”, issued on Jan. 8, 1980; U.S. Pat. No. 4,160,180, having the title “ROTOR LAMINATION SUPPORT FOR VERTICAL HYDROGENERATOR”, issued on Jul. 3, 1979; U.S. Pat. No. 4,110,652, having the title “Mounting assembly for laminated rotor rim of dynamoelectric generator rotatable about inclined shaft”, issued on Aug. 29, 1978; U.S. Pat. No. 3,529,193, having the title “ROTOR FOR ELECTRIC MACHINE WITH VERTICAL SHAFT”, issued on Sep. 15, 1970; U.S. Pat. No. 3,470,404, having the title “ROTORS FOR ROTATING ELECTRIC MACHINES”, issued on Sep. 30, 1969; U.S. Pat. No. 3,112,420, having the title “Rotor construction for waterwheel driven electrical generator”, issued on Nov. 26, 1963; U.S. Pat. No. 3,046,426, having the title “Rotor spider for electrical machines”, issued on Jul. 24, 1962; U.S. Pat. No. 2,994,793, having the title “Dynamoelectric machine”, issued on Aug. 1, 1962; U.S. Pat. No. 1,817,054, having title “Large, high speed rotor”, issued on Aug. 4, 1931; Japanese patent document number 60-102829; and Japanese patent document number 54102501.
- The components disclosed in the patents, patent applications, patent publications, and other documents disclosed or incorporated by reference herein, may possibly be used in possible embodiments of the present invention, as well as equivalents thereof.
- The purpose of the statements about the technical field is generally to enable the Patent and Trademark Office and the public to determine quickly, from a cursory inspection, the nature of this patent application. The description of the technical field is believed, at the time of the filing of this patent application, to adequately describe the technical field of this patent application. However, the description of the technical field may not be completely applicable to the claims as originally filed in this patent application, as amended during prosecution of this patent application; and as ultimately allowed in any patent issuing from this patent application. Therefore, any statements made relating to the technical field are not intended to limit the claims in any manner and should not be interpreted as limiting the claims in any manner.
- The appended drawings in their entirety, including all dimensions, proportions and/or shapes in at least one exemplification of the invention, are accurate and are hereby included by reference into this specification.
- The background information is believed, at the time of the filing of this patent application, to adequately provide background information for this patent application. However, the background information may not be completely applicable to the claims as originally filed in this patent application, as amended during prosecution of this patent application, and as ultimately allowed in any patent issuing from this patent application. Therefore, any statements made relating to the background information are not intended to limit the claims in any manner and should not be interpreted as limiting the claims in any manner.
Claims (20)
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|---|---|---|---|
| US18/537,203 US12316177B2 (en) | 2020-12-14 | 2023-12-12 | Method of repairing a hydrogenerator |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US16/974,278 US11870310B2 (en) | 2020-12-14 | 2020-12-14 | Method of repairing a hydrogenerator |
| US18/537,203 US12316177B2 (en) | 2020-12-14 | 2023-12-12 | Method of repairing a hydrogenerator |
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| US16/974,278 Continuation US11870310B2 (en) | 2020-12-14 | 2020-12-14 | Method of repairing a hydrogenerator |
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| US4327303A (en) * | 1980-09-29 | 1982-04-27 | Siemens-Allis, Inc. | Rotor assembly for a dynamoelectric machine |
| US5347880A (en) * | 1992-11-23 | 1994-09-20 | Harnischfeger Corporation | Method and apparatus for servicing a gear assembly |
| US20110278994A1 (en) * | 2010-05-13 | 2011-11-17 | Hitachi, Ltd. | Rotor of rotating electrical machine |
| US20200331103A1 (en) * | 2017-12-04 | 2020-10-22 | Cnc Onsite A/S | Method for Repairing a Gear and Processing Machine for Carrying Out the Method |
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| US20220190694A1 (en) | 2022-06-16 |
| US12316177B2 (en) | 2025-05-27 |
| US11870310B2 (en) | 2024-01-09 |
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